NORSAT 4, 62702
Orbit data source: Space-Track
NORSAT 4, 62702 is a payload satellite owned by NSC (NO) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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62702 intel report (Beta)
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Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
UTIAS-SFL
Mission
Operational Civil Com/Tech
Bus & Motor
DEFIANT, Unknown motor
Mass
35 kg wet, 35 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.6 m
Radar Cross Section
0.165 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 NORSAT 4
1 62702U 25009CX 26081.22822026 .00002594 00000-0 24428-3 0 9997
2 62702 97.7080 161.4658 0001289 25.6743 334.4541 14.94695467 64377Epoch: 2026-03-22T05:28Z
TLE epoch observation values (Epoch: 2026-03-22T05:28:38.230Z)
Latitude
-0.00005°
Longitude
-100.43108°
Altitude
585.556 km
Speed
7.568 km/s
True Right ascension
10h 45m 51s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
18:55:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
581.228 km
Perigee altitude
579.434 km
Semi-major axis
6,958.468 km
Eccentricity
0.00013
Inclination
97.708°
RAAN
161.4658°
Arg. of periapsis
25.6743°
True anomaly
334.44773°
Mean anomaly
334.4541°
Eccentric anomaly
334.45091°
Mean motion
3.73915 °/min
Orbital period
96.28 mins
BSTAR
0.00024428
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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.NORSAT 4 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-03-22 17:19:00.879Z | 54.472° ENE | 2026-03-22 17:21:00.879Z | 90.486° ESE | 20.283° | 2026-03-22 17:24:00.879Z | 142.22° SSE |
| 5 mins | 2026-03-22 18:55:00.879Z | 326.048° NNW | 2026-03-22 18:57:00.879Z | 278.123° WNW | 24.564° | 2026-03-22 19:00:00.879Z | 231.609° WSW |
| 6 mins | 2026-03-23 05:43:00.879Z | 199.305° SSW | 2026-03-23 05:45:00.879Z | 253.052° W | 35.473° | 2026-03-23 05:49:00.879Z | 334.468° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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